FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular to the designs of multi-propeller aircrafts. Aerial electrolifting aircraft comprises fuselage, at least four propellers, each of which is kinematically connected with controlled electric drive shaft arranged on rigid platform located above fuselage. Fuselage is rigidly fixed on a bracket which is pivotally connected to the platform by means of bearings. Fuselage is also connected to rigid platform by piston damper. Electric drives of the propellers are connected to the power supply source kinematically connected to the engine output shaft.
EFFECT: providing vertical and track control of aircraft due to change of rotation speed of propellers while providing aerodynamic stability of fuselage.
1 cl, 2 dwg
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